In this paper, I present the design of Mira 2, a small-scale, liquid bipropellant rocket engine, with a specific focus on its oxidizer-centered pintle injector. Building upon the valuable lessons and insights gained from the empirical testing of its predecessor, Mira 1, the Mira 2 engine incorporates several improvements and...
This script takes a short list of inputs as design requirements and recommends several possible engine configurations that will fit within the specified criteria. Many of the parameters can be directly solved from the specified inputs via basic relationships and equations; however, some output parameters require iteration across a range...